A gas turbine engine is mounted on an aircraft which can attain a maximum altitude of 11 km from
sea level. The combustor volume of this engine is decided based on conditions at
(A) sea level (B) 8 km altitude (C ) 5.5 km altitude (D) 11 km altitude
Official Answer Key:
0.0
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2013 Q.22)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Structural Mechanics** under *Aerospace Structures* (1 Mark, NAT).
**2. Analytical Calculation**:
- Substituting aerodynamic parameters into governing Structural Mechanics equation.
**3. Final Answer**:
Acceptable official numerical value is **0.0**.
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